View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 33504U 26038.73673469 +.00000000 +00000-0 +29417-3 0 00008
2 33504 82.4325 306.9966 0008911 265.8374 94.1855 15.42533662 03
| Epoch (UTC): | 07 February 2026 17:40:53 |
| Eccentricity: | 0.0008911 |
| inclination: | 82.4325° |
| perigee height: | 433 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 306.9966° |
| argument of perigee: | 265.8374° |
| revolutions per day: | 15.42533662 |
| mean anomaly at epoch: | 94.1855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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